This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Kartukov. Developed in: 1962-66. Application: Soyuz 7K-OK, Soyuz 7KT-OK, Soyuz 7K-T. Used on spacecraft: Soyuz 7K-OK, Soyuz 7KT-OK, Soyuz 7K-T. Propellants: Solid Thrust(vac): 80,100 kgf. Thrust(vac): 785.00 kN. Country: Russia. Status: Out of Production. Comments: Thrust 76 tf at cutout - 80.1tf at ignition.
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Last update 12 March 2001.
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© Mark Wade, 2001 .